EP 2278125 B1 20170927 - Turbine nozzle assembly including radially-compliant spring member for gas turbine engine
Title (en)
Turbine nozzle assembly including radially-compliant spring member for gas turbine engine
Title (de)
Turbinenleitschaufelanordnung mit radial anpassungsfähiger Feder für ein Gasturbinentriebwerk
Title (fr)
Aube statorique avec ressort radialement adaptable pour turbine à gaz
Publication
Application
Priority
US 50690409 A 20090721
Abstract (en)
[origin: EP2278125A2] Embodiments of a turbine nozzle assembly (58) are provided for deployment within a gas turbine engine (GTE 20) including a first GTE-nozzle mounting interface (101). In one embodiment, the turbine nozzle assembly includes a turbine nozzle flowbody, a first mounting flange (98) configured to be mounted to the first GTE-nozzle mounting interface, and a first radially-compliant spring member (131) coupled between the turbine nozzle flowbody and the first mounting flange (98). The turbine nozzle flowbody has an inner nozzle endwall (92) and an outer nozzle endwall (90), which is fixedly coupled to the inner nozzle endwall (92) and which cooperates therewith to define a flow passage (96) through the turbine nozzle flowbody. The first radially-compliant spring member (131) accommodates relative thermal movement between the turbine nozzle flowbody and the first mounting flange (98) to alleviate thermomechanical stress during operation of the GTE (20).
IPC 8 full level
F01D 11/02 (2006.01); F01D 9/04 (2006.01)
CPC (source: EP US)
F01D 9/02 (2013.01 - EP US); F01D 9/042 (2013.01 - EP US); F05D 2260/38 (2013.01 - EP US); F05D 2260/941 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR
DOCDB simple family (publication)
EP 2278125 A2 20110126; EP 2278125 A3 20130306; EP 2278125 B1 20170927; US 2011020118 A1 20110127; US 8388307 B2 20130305
DOCDB simple family (application)
EP 10162759 A 20100512; US 50690409 A 20090721